Embodiments of the invention provide an improved process for depositing tungsten-containing materials. The process utilizes soak processes and vapor deposition processes, such as atomic layer deposition (ALD) to provide tungsten films having significantly improved surface uniformity and production level throughput. In one embodiment, a method for forming a tungsten-containing material on a substrate is provided which includes positioning a substrate within a process chamber, wherein the substrate contains an underlayer disposed thereon, exposing the substrate sequentially to a tungsten precursor and a reducing gas to deposit a tungsten nucleation layer on the underlayer during an ALD process, wherein the reducing gas contains a hydrogen/hydride flow rate ratio of about 40:1, 100:1, 500:1, 800:1, 1,000:1, or greater, and depositing a tungsten bulk layer on the tungsten nucleation layer. The reducing gas contains a hydride compound, such as diborane, silane, or disilane.
Legal claims defining the scope of protection, as filed with the USPTO.
1. A method for forming a tungsten-containing material on a substrate, comprising: positioning a substrate within a process chamber, wherein the substrate comprises an underlayer disposed thereon; exposing the substrate sequentially to a tungsten precursor and a reducing gas to deposit a tungsten nucleation layer on the underlayer during an atomic layer deposition process, wherein the reducing gas comprises a hydrogen/hydride flow rate ratio of about 500:1 or greater; and depositing a tungsten bulk layer on the tungsten nucleation layer.
2. The method of claim 1 , wherein the reducing gas comprises a hydride compound selected from the group consisting of silane, disilane, diborane, phosphine, derivatives thereof, and combinations thereof.
3. The method of claim 2 , wherein the reducing gas comprises diborane.
4. The method of claim 2 , wherein the reducing gas comprises silane or disilane.
5. The method of claim 1 , wherein the hydrogen/hydride flow rate ratio of the reducing gas is about 800:1 or greater.
6. The method of claim 5 , wherein the hydrogen/hydride flow rate ratio of the reducing gas is about 1,000:1 or greater.
7. The method of claim 1 , wherein the hydride compound comprises a flow rate within a range from about 1 sccm to about 40 sccm.
8. The method of claim 7 , wherein the reducing gas comprises hydrogen having a flow rate within a range from about 1 slm to about 20 slm.
9. The method of claim 8 , wherein the flow rate of the hydride compound is within a range from about 3 sccm to about 30 sccm and the hydrogen comprises a flow rate within a range from about 3 slm to about 15 slm.
10. The method of claim 9 , wherein the flow rate of the hydride compound is within a range from about 5 sccm to about 15 sccm and the hydrogen comprises a flow rate within a range from about 5 slm to about 10 slm.
11. The method of claim 1 , wherein the substrate is heated to a temperature within a range from about 350° C. to about 420° C.
12. The method of claim 1 , further comprising exposing the underlayer to a pre-soak gas comprising the reducing agent during a pre-soak process, wherein the underlayer is exposed to the reducing agent for a time period within a range from about 5 seconds to about 60 seconds.
13. The method of claim 12 , wherein the time period is within a range from about 10 seconds to about 30 seconds.
14. The method of claim 1 , further comprising exposing the tungsten nucleation layer to a post-soak gas comprising the reducing agent during a post-soak process, wherein the tungsten nucleation layer is exposed to the reducing agent for a time period within a range from about 5 seconds to about 60 seconds.
15. The method of claim 14 , wherein the time period is within a range from about 10 seconds to about 30 seconds.
16. The method of claim 1 , wherein the tungsten bulk layer has a resistivity measured across the substrate of about 10 μΩ-cm or less.
17. The method of claim 16 , wherein the resistivity is about 8 μΩ-cm or less.
18. The method of claim 1 , wherein the underlayer is a barrier layer and comprises a material selected from the group consisting of metallic titanium, titanium nitride, metallic tantalum, tantalum nitride, ruthenium, nickel, cobalt, metallic tungsten, tungsten nitride, silicides thereof, derivatives thereof, alloys thereof, and combinations thereof.
19. The method of claim 18 , wherein the tungsten bulk layer is deposited by a chemical vapor deposition process.
20. A method for forming a tungsten-containing material on a substrate, comprising: positioning a substrate within a process chamber, wherein the substrate comprises an underlayer disposed thereon; exposing the substrate sequentially to a tungsten precursor and a reducing gas to deposit a tungsten nucleation layer on the underlayer during an atomic layer deposition process, wherein the reducing gas comprises a hydrogen/diborane flow rate ratio of about 100:1 or greater; and depositing a tungsten bulk layer on the tungsten nucleation layer.
21. The method of claim 20 , wherein the hydrogen/diborane flow rate ratio of the reducing gas is about 800:1 or greater.
22. A method for forming a tungsten-containing material on a substrate, comprising: positioning a substrate within a process chamber, wherein the substrate comprises an underlayer disposed thereon; exposing the underlayer to a pre-soak gas comprising diborane during a pre-soak process; exposing the substrate sequentially to a tungsten precursor and a reducing gas to deposit a tungsten nucleation layer on the underlayer during an atomic layer deposition process, wherein the reducing gas comprises a hydrogen/diborane flow rate ratio of about 100:1 or greater; exposing the substrate to a post-soak gas comprising diborane during a post-soak process; and depositing a tungsten bulk layer on the tungsten nucleation layer.
23. The method of claim 22 , wherein the hydrogen/diborane flow rate ratio of the reducing gas is about 500:1 or greater.
24. The method of claim 23 , wherein the hydrogen/diborane flow rate ratio of the reducing gas is about 800:1 or greater.
Cooperative Patent Classification codes for this invention. Click any code to explore related patents in that topic.
May 15, 2008
June 21, 2011
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